Lockheed C-5M, Техническое руководство

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NAV MFDU (if installed)
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NAV CCP (if installed)
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NAV MCDU (if installed)
(17) Navigator circuit breaker panel No. 2, AVIONICS DC BUS 2A
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VIA 2
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AIU 2
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COPILOT CCD
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COPILOT CNP
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COPILOT RIGHT MFDU
(18) Navigator circuit breaker panel No. 2, AVIONICS AC BUS 2 PH A
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BAU 2
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AVIONICS AC BUS 2A
(19) Navigator circuit breaker panel No. 2, AVIONICS DC BUS 2B
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BSIU 2
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FE MFDU
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FE CCP
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OBS MCDU
(20) Navigator circuit breaker panel No. 2, AVIONICS AC BUS 2A PH A
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VIA 2 FAN
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AIU 2 FAN
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26 VAC AVIONICS TRANS
d. Ensure VIA/AIU ALT POWER switch (Figure 1-24, 2) is in NORMAL.
Do not apply force or hang any items on control wheel yoke. Failure to comply will result in failures and
calibration errors of control wheel hub sensors.
e. Close ground switches on the pilot emergency circuit breaker panel (Figure 1-21), ensuring that ground switches on
the pilot emergency circuit breaker panel are closed at least 5 seconds before ground switches on navigator circuit
breaker panels No. 1 and No. 2.
f. Close ground switches on navigator circuit breaker panels No. 2, then No. 1 (Figure 1-21).
g. If pilot MASTER CAUTION fails to reset, open and reset RIU No. 1 circuit breaker on pilot lower emergency circuit
breaker panel, EMERGENCY DC BUS. Otherwise, proceed to next step.
TO 1C-5M-2-1
1-21